A side-by-side dual-launch spacecraft arrangement is provided. The arrangement may include a dual-launch adaptor, a first spacecraft, and a second spacecraft. The first spacecraft and the second spacecraft may be mounted on the dual-launch adaptor and may be arranged side by side on the dual-launch adaptor. An aspect ratio of each of the first and second spacecraft may be within a range of 0.55 and 0.8.
SIDE-BY-SIDE DUAL-LAUNCH ARRANGEMENT WITH IMPROVED PAYLOAD COMPATIBILITY
NEBENEINANDER ANGEORDNETE DUALABSCHUSSANORDNUNG MIT VERBESSERTER NUTZLASTKOMPATIBILITÄT
AGENCEMENT DE LANCEMENT DOUBLE CÔTE À CÔTE AVEC COMPATIBILITÉ DE CHARGE AMÉLIORÉE
2019-04-10
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Side-by-side dual-launch arrangement with improved payload compatibility
Europäisches Patentamt | 2017
|SIDE-BY-SIDE DUAL-LAUNCH ARRANGEMENT WITH IMPROVED PAYLOAD COMPATIBILITY
Europäisches Patentamt | 2017
|